本文主要目的是針對TUU SAT.1小微衛星的任務需求,且考慮衛星軌道、熱傳、太空環境、研製成本等因素的限制,決定採用重力梯度穩定被動控制方法配合主動的磁力矩控制方式,進行TUU SAT.1小微衛星的姿態控制設計,而控制器的原理採用模糊理論。 In this paper, the attitude controller of TUU-SAT is designed, After we have considered these factors of orbit, thermal, Space environment and cost, the Passive Gravity Gradient Stabilization type is adopted, and where the magnetic-torquers produced magnetic field to affect the earth's magnetic field, then grow a magnetic force to correct the attitude of Satellite. The attitude controller is based on fuzzy logic control.
關聯:
中國航空太空學會學刊=Transactions of the Aeronautical and Astronautical Society of the Republic of China 29(2),頁109-114